Conducted ota test fixture

ABSTRACT

Systems and methods relating to performing individual transmit and/or receive measurements for each antenna element in an antenna array implemented on an Substrate Integrated Antenna Array (SIAA) are disclosed. In some embodiments, an SIAA comprises a substrate, one or more antenna elements at a surface of the substrate, and an electrically conductive via fence having a first side electrically coupled to ground within the substrate and a second side at the surface of the substrate, the electrically conductive via fence separately circumscribing each antenna element of the one or more antenna elements within the substrate. The SIAA enables the use of a respective test structure to perform per-antenna element measurements.

This application is a divisional of U.S. application Ser. No.15/325,156, filed Jan. 10, 2017, which is a 35 U.S.C. § 371 nationalphase filing of International Application No. PCT/IB2016/056260, filedOct. 18, 2016, the disclosures of which are incorporated herein byreference in their entireties.

TECHNICAL FIELD

The present disclosure relates to a substrate integrated antenna arrayand, more specifically, to obtaining measurements for individual antennaelements in such an array.

BACKGROUND

Future generation (e.g., Fifth Generation (5G)) cellular communicationsnetworks that operate on millimeter frequencies will use a large numberof antennas, particularly at the base stations but potentially also atthe wireless devices. The antennas utilized by a particular radio node(e.g., a base station or a wireless device) are implemented as anantenna array. The number of antenna elements in such an antenna arrayis expected to be 128 or even higher. Further, at millimeterfrequencies, the antenna array is likely to be integrated with the RadioFrequency (RF) components on a single substrate (e.g., a single PrintedCircuit Board (PCB)). A substrate on which the antenna array and, insome implementations, the RF components are integrated is referred toherein as a Substrate Integrated Antenna Array (SIAA).

One issue that will arise for an integrated antenna system with noaccess to connectors to perform legacy testing is that testingrequirements such as, for example, output power, Error Vector Magnitude(EVM), and Adjacent Channel Leakage Ratio (ACLR) will not always befeasible using traditional testing schemes, i.e., conducted testing thatutilizes connectors or cables to each transceiver chain. Conductedtesting schemes are also referred to herein as connector-based testingschemes. One alternative testing scheme is a radiated testing schemesuch as a testing scheme that utilizes an anechoic test chamber.However, radiated testing such that those using an anechoic test chamberrequire long test times since each antenna element must be testedseparately. In addition, radiated testing schemes do not isolatespecific antenna elements or transceiver chains in order to investigatebroken or degraded antenna elements or transceiver chains.

While conducted testing schemes may be used to separately testtransceiver chains, these testing schemes require separate physicalconnectors to each transceiver chain. However, a conducted testingscheme would be more challenging for SIAAs having a large number oftransceiver chain and associated physically small antenna elements sincephysical connectors to each individual transceiver chain would bechallenging. Further, a conducted testing scheme usually requiresdisconnecting the antenna element from the radio analog parts. Althoughthis test enables observations of the individual radio parts, itintroduces undesirable, lossy, and complex circuits. Also, since theantenna elements are disconnected, the conducted testing scheme does notinclude the antenna elements as part of the test and, therefore, doesnot provide test coverage of the antenna element.

Even if connector-based test mechanisms are possible, they may not bethe best solution for an SIAA or other antenna integrated radio. Athigher frequencies (millimeter wave), connector-based test mechanismsare difficult to implement. Further, the connectors provide unnecessaryloss, and this loss has a larger impact at high frequencies. Stillfurther, at times, the connectors utilized for the connector-basedtesting mechanism can be larger in size than the antenna element itself;therefore, the connector-based testing mechanism can be a bulkysolution. In some implementations (e.g., mmWave), the needed connectortype or size may not exist or may be challenging to manufacture.

Thus, connector-less testing mechanisms for testing an SIAA, e.g.,during design and manufacturing, are desired. However, as noted above,conventional over-the-air testing mechanisms are less than idealbecause, e.g., they require longer test times, which is particularlyproblematic as the number of antenna elements increases as the systemwould have to cycle through testing each antenna element on its own.Therefore, there is a need for a connector-less testing mechanism thatenables testing of individual antenna elements and/or radio signal pathsfor an SIAA and, in particular, an SIAA that includes an antenna arrayincluding a large number of antenna elements such as those used formillimeter wave frequencies.

SUMMARY

Systems and methods relating to performing individual transmit and/orreceive measurements for each antenna element in an antenna arrayimplemented on a Substrate Integrated Antenna Array (SIAA) aredisclosed. In some embodiments, an SIAA comprises a substrate, one ormore antenna elements at a surface of the substrate, and an electricallyconductive via fence having a first side electrically coupled to groundwithin the substrate and a second side at the surface of the substrate,the electrically conductive via fence separately circumscribing eachantenna element of the one or more antenna elements within thesubstrate. The SIAA enables the use of a respective test structure toperform per-antenna element measurements.

In some embodiments, the one or more antenna elements comprise aplurality of antenna elements. In some embodiments, the antenna elementsare structures on the surface of the substrate. In other embodiments,the antenna elements are slot antenna elements formed in a metal groundplane on the surface of the substrate.

In some embodiments, the electrically conductive via fence comprises aplurality of electrically conductive vias each having a first endcoupled to ground within the substrate and a second end at the surfaceof the substrate. The plurality of electrically conductive vias arepositioned in the substrate such that each antenna element of the one ormore antenna elements is separately circumscribed by a respective subsetof the plurality of electrically conductive vias.

In some embodiments, the electrically conductive via fence is acontinuous structure.

In some embodiments, the substrate comprises a mechanical alignmentfeature. Further, in some embodiments, the mechanical alignment featurecomprises at least one of a group consisting of: a groove in the surfaceof the substrate around a periphery of the substrate, a ridge on thesurface of the substrate around a periphery of the substrate, aplurality of pins on the surface of the substrate, and a plurality ofholes into the surface of the substrate.

In some embodiments, the substrate is a Printed Circuit Board (PCB).

In some embodiments, the SIAA further comprises a dielectric on asurface of the one or more antenna elements opposite the substrate. Insome embodiments, a thickness of the dielectric is less than λ/4, whereλ is a wavelength of a carrier frequency to be transmitted or receivedby the SIAA.

Embodiments of a system comprising an SIAA and a test fixture assemblyare also disclosed. In some embodiments, the SIAA comprises a substrateand one or more antenna elements at a surface of the substrate The testfixture assembly comprises one or more cavities formed by one or morematerials providing isolation between the plurality of antenna elements.The one or more materials may include an electrically conductivematerial, a convective coated non-conductive material with a skin depth(i.e., thickness of the convective coating) that is sufficient toprovide isolation between the plurality of antenna elements, one or morenon-conductive materials that are doped to provide electricalconductivity, or the like. The test fixture assembly is positioned onthe surface of the substrate of the SIAA such that, for each cavity ofthe one or more cavities, sidewalls of the cavity circumscribe arespective one of the plurality of antenna elements such that the one ormore cavities electrically isolate the one or more antenna elements.

In some embodiments, the one or more antenna elements comprise aplurality of antenna elements, and the one or more cavities comprise aplurality of cavities. In some embodiments, the antenna elements arestructures on the surface of the substrate. In other embodiments, theantenna elements are slot antenna elements formed in a metal groundplane on the surface of the substrate.

In some embodiments, the SIAA further comprises an electricallyconductive via fence having a first side electrically coupled to groundwithin the substrate and a second side at the surface of the substrate.The electrically conductive via fence separately circumscribes eachantenna element of the one or more antenna elements within thesubstrate. The test fixture assembly is positioned on the surface of thesubstrate of the SIAA such that, for each cavity of the one or morecavities, the sidewalls of the cavity are aligned with and electricallycoupled to sections of the electrically conductive via fence thatcircumscribe a respective one of the plurality of antenna elements suchthat the via fence and the one or more cavities electrically isolate theone or more antenna elements.

In some embodiments, the sidewalls of the cavity are in physical contactwith the sections of the electrically conductive via fence thatcircumscribe the respective one of the one or more antenna elements.

In some embodiments, the electrically conductive via fence comprises aplurality of electrically conductive vias each having a first endcoupled to ground within the substrate and a second end at the surfaceof the substrate. The plurality of electrically conductive vias arepositioned in the substrate such that each antenna element of the one ormore antenna elements is separately circumscribed by a respective subsetof the plurality of electrically conductive vias. The test fixtureassembly is positioned on the surface of the substrate of the SIAA suchthat, for each cavity of the one or more cavities, sidewalls of thecavity are aligned with and electrically coupled to the subset of theplurality of electrically conductive vias that circumscribe a respectiveone of the one or more antenna elements such that the via fence and theone or more cavities electrically isolate the one or more antennaelements. In some embodiments, the sidewalls of the cavity are inphysical contact with the subset of the plurality of electricallyconductive vias that circumscribe the respective one of the one or moreantenna elements.

In some embodiments, the SIAA further comprises a dielectric on asurface of the one or more antenna elements opposite the substrate. Insome embodiments, a thickness of the dielectric is less than λ/4, whereλ is a wavelength of a carrier frequency to be transmitted or receivedby the SIAA.

In some embodiments, the system further comprises a mechanical alignmentmechanism that aligns the test fixture assembly with the SIAA such thatthe one or more cavities in the test fixture assembly are aligned withthe one or more antenna elements, respectively. In some embodiments, themechanical alignment mechanism comprises a groove around a periphery ofone of the SIAA and the test fixture assembly and a ridge around aperiphery of the other one of the SIAA and the test fixture assembly.

In some embodiments, the test fixture assembly further comprises one ormore sensors in the one or more cavities, respectively. In someembodiments, the system further comprises a controller that processessignals output by the one or more sensors during transmission of signalsfrom the one or more antenna elements to perform one or moremeasurements for each of the one or more antenna elements. In someembodiments, the one or more measurements comprise at least one ofamplitude error, phase error, output power, error vector magnitude, andadjacent channel leakage ratio.

In some embodiments, the system further comprises a controller thatgenerates signals that are injected into the one or more cavities by theone or more sensors and processes one or more received signals output bythe one or more antenna elements during reception of the signals fromthe one or more sensors to perform one or more receive measurements foreach of the one or more antenna elements. In some embodiments, the oneor more receive measurements comprise at least one of a group consistingof: noise figure and receive sensitivity.

In some embodiments, a method comprises performing one or moremeasurements for each of one or more antenna elements on an SIAA using atest fixture assembly comprising one or more cavities formed by one ormore materials providing isolation between the plurality of antennaelements. The one or more materials may include an electricallyconductive material, a convective coated non-conductive material with askin depth (i.e., thickness of the convective coating) that issufficient to provide isolation between the plurality of antennaelements, one or more non-conductive materials that are doped to provideelectrical conductivity, or the like. The test fixture assembly beingpositioned on a surface of the SIAA such that, for each cavity of theone or more cavities, sidewalls of the cavity circumscribe a respectiveone of the one or more antenna elements such that the one or morecavities electrically isolate the one or more antenna elements. Themethod further comprises utilizing the one or more measurements.

In some embodiments, utilizing the one or more measurements comprisesutilizing the one or more measurements to calibrate the one or moreantenna elements.

In some embodiments, utilizing the one or more measurements comprisesproviding information related to the one or more measurements along withthe SIAA to another entity, wherein the information comprises at leastone of a group consisting of: the one or more measurements andinformation derived from the one or more measurements.

In some embodiments, a method comprises obtaining an SIAA andinformation related to one or more measurements for each of one or moreantenna elements on the SIAA, and utilizing the information.

In some embodiments, the one or more measurements for each of the one ormore antenna elements on the SIAA were performed using a test fixtureassembly comprising one or more cavities formed by one or more materialsproviding isolation between the plurality of antenna elements. The oneor more materials may include an electrically conductive material, aconvective coated non-conductive material with a skin depth (i.e.,thickness of the convective coating) that is sufficient to provideisolation between the plurality of antenna elements, one or morenon-conductive materials that are doped to provide electricalconductivity, or the like. While the one or more measurements for eachof the one or more antenna elements were performed, the test fixtureassembly was positioned on a surface of the SIAA such that, for eachcavity of the one or more cavities, sidewalls of the cavity circumscribea respective one of the one or more antenna elements such that the oneor more cavities electrically isolate the one or more antenna elements.

In some embodiments, the SIAA comprises a substrate, one or more antennaelements at a surface of the substrate, and an electrically conductivevia fence having a first side electrically coupled to ground within thesubstrate and a second side at the surface of the substrate. Theelectrically conductive via fence separately circumscribes each antennaelement of the one or more antenna elements within the substrate.

In some embodiments, the substrate comprises a mechanical alignmentfeature.

In some embodiments, the SIAA further comprises a dielectric on asurface of the one or more antenna elements opposite the substrate. Insome embodiments, a thickness of the dielectric is less than λ/4, whereλ is a wavelength of a carrier frequency to be transmitted or receivedby the SIAA.

Those skilled in the art will appreciate the scope of the presentdisclosure and realize additional aspects thereof after reading thefollowing detailed description of the embodiments in association withthe accompanying drawing figures.

BRIEF DESCRIPTION OF THE DRAWINGS

The accompanying drawing figures incorporated in and forming a part ofthis specification illustrate several aspects of the disclosure, andtogether with the description serve to explain the principles of thedisclosure.

FIG. 1 illustrates a system including an Substrate Integrated AntennaArray (SIAA) and a test fixture assembly for obtaining per antennaelement measurements according to some embodiments of the presentdisclosure;

FIG. 2 illustrates one example variation of the system of FIG. 1 inwhich a dielectric structure is included on the SIAA over the antennaelements;

FIGS. 3A through 3C illustrate a cross-sectional view and two top-downviews of two example embodiments of the SIAA of FIG. 1 according to someembodiments of the present disclosure;

FIGS. 4A and 4B illustrate a cross-sectional view and a bottom-up viewof the test fixture assembly of FIG. 1 according to some embodiments ofthe present disclosure;

FIG. 5 illustrates the SIAA according to some other embodiments in whichthe antenna array is a slotted antenna array;

FIG. 6 illustrates a system including the SIAA of FIG. 5 and a testfixture assembly for obtaining per antenna element measurementsaccording to some embodiments of the present disclosure;

FIG. 7 illustrates a process relating to the use of the SIAA and testfixture assembly according to some embodiments of the presentdisclosure; and

FIG. 8 illustrates a process relating to the use of the SIAA and testfixture assembly according to some other embodiments of the presentdisclosure.

DETAILED DESCRIPTION

The embodiments set forth below represent information to enable thoseskilled in the art to practice the embodiments and illustrate the bestmode of practicing the embodiments. Upon reading the followingdescription in light of the accompanying drawing figures, those skilledin the art will understand the concepts of the disclosure and willrecognize applications of these concepts not particularly addressedherein. It should be understood that these concepts and applicationsfall within the scope of the disclosure and the accompanying claims.

For Substrate Integrated Antenna Array (SIAA) systems, the fullradiation pattern may not currently be required to meet Third GenerationPartnership Project (3GPP) conformance requirements. The testrequirement for Equivalent Isotropically Radiated Power (EIRP)/EffectiveIsotropic Sensitivity (EIS) is for one point on the main beam at varioussteering angles and not a full 360 degree radiation pattern. This meansthat today's antenna testing ranges are not the only solution fortesting SIAA base stations in order to meet the minimum requirement.

Systems and methods relating to performing individual transmit and/orreceive measurements for each antenna element in an antenna arrayimplemented on an AAS are disclosed. As used herein, an AASSIAA is asubstrate (e.g., a Printed Circuit Board (PCB)) on which multipleantenna elements of an antenna array are implemented. In someembodiments, Radio Frequency (RF) components (e.g., components of a RFtransmitter and/or a RF receiver) are also implemented on the SIAA.

In this regard, FIG. 1 illustrates a system 10 in which a test fixtureassembly 12 is utilized to perform transmit and/or receive measurementsfor individual antenna elements 14 of an SIAA 16 according to someembodiments of the present disclosure. As illustrated, the SIAA 16includes a substrate 18. The substrate 18 may be, for example, a PCB,but is not limited thereto. Other types of substrates 18 may be used. Inthis embodiment, the antenna elements 14 are structures on a surface ofthe SIAA 16. For simplicity and ease of discussion, in the illustratedexample, there are three antenna elements 14, which are referenced asantenna elements 14-1, 14-2, and 14-3. However, it should be noted thatthe SIAA 16 may include many antenna elements 14 (e.g., 128 or more).The antenna elements 14 are formed of any suitable material such as, forexample, an electrically conductive material, e.g., a metal. While metalis one example, other materials may be used. For example, a materialthat is suitable for a dielectric radiating antenna may be used. Asdiscussed below with respect to FIGS. 5 and 6, in some otherembodiments, the antenna elements 14 are slots forming respective slotantenna elements.

The SIAA 16 also includes an electrically conductive via fence 20. Afirst side of the electrically conductive via fence 20 is coupled to(e.g., physically connected to) ground within the substrate 18. In thisparticular example, the first side of the electrically conductive viafence 20 is coupled to a ground plate 22 within the substrate 18. Asecond side of the electrically conductive via fence 20 is at thesurface of the substrate 18. In some embodiments, the second side of theelectrically conductive via fence 20 is exposed at the surface of thesubstrate 18 or electrically and physically connected to a contact onthe surface of the substrate 18. However, in some embodiments, thesecond side of the electrically conductive via fence 20 is not exposedat the surface of the substrate 18 but is sufficiently near the surfaceof the substrate 18 to, together with the test fixture assembly 12,enable electrical isolation of the antenna elements 14.

In some embodiments, the electrically conductive via fence 20 is formedby many vias, or holes, in the substrate 18 that are filled with anelectrically conductive material (e.g., a metal). In some otherembodiments, the electrically conductive via fence 20 is formed bytrenches formed into the surface of the substrate 18 that are filledwith an electrically conductive material such that the electricallyconductive via fence 20 is a continuous structure. Further, in someembodiments, the SIAA 16 includes a contact(s) on the surface of thesubstrate 18 over the electrically conductive via fence 20 to enableelectrical and, in this example, physical contact between theelectrically conductive via fence 20 and the test fixture assembly 12,as described below.

The electrically conductive via fence 20 separately circumscribes eachof the antenna elements 14 within the substrate 18. In other words, theelectrically conductive via fence 20 includes a first section thatcircumscribes the antenna element 14-1, a second section thatcircumscribes the antenna element 14-2, and a third section thatcircumscribes the antenna element 14-3. As discussed below in detail,together with the test fixture assembly 12, the electrically conductivevia fence 20 forms a multi-cavity structure that electrically isolateseach individual antenna element 14 such that measurements can beperformed on the antenna elements 14 individually.

The test fixture assembly 12 includes a fixture 24, or supportstructure, and a number of cavities 26 formed by one or more materials28 within the fixture 24 providing isolation between the plurality ofantenna elements. The one or more materials 28 may include anelectrically conductive material (e.g., a metal), a convective coatednon-conductive material with a skin depth (i.e., thickness of theconvective coating) that is sufficient to provide isolation between theplurality of antenna elements, one or more non-conductive materials thatare doped to provide electrical conductivity, or similar material(s)having a low dielectric constant or suitable skin depth. In thisexample, there are three cavities 26, which are referenced as cavities26-1, 26-2, and 26-3.

The test fixture assembly 12 is positioned on the SIAA 16 such that thecavities 26-1, 26-2, and 26-3 are aligned with the antenna elements14-1, 14-2, and 14-3, respectively. More specifically, the test fixtureassembly 12 is positioned on the SIAA 16 such that sidewalls 30 of thecavities 26-1, 26-2, and 26-3 are aligned with and electrically coupledto the sections of the electrically conductive via fence 20 thatcircumscribe the respective antenna elements 14-1, 14-2, and 14-3. Asdiscussed above, one side (e.g., the top side in the illustratedexample) of the electrically conductive via fence 20 is at the surfaceof the substrate 18 of the SIAA 16 to thereby enable electrical and, inthis example, physical contact between the electrically conductive viafence 20 and the sidewalls 30 of the cavities 26. The cavities 26 havean appropriate geometry with respect to the electrically conductive viafence 20 that enables the cavities 26 together with the electricallyconductive via fence 20 to electrically isolate the antenna elements 14.Specifically, the cavity 26-1 and the section of the electricallyconductive via fence 20 that circumscribes the antenna element 14-1electrically isolate the antenna element 14-1. In the same manner, thecavities 26-2 and 26-3 together with the respective sections of theelectrically conductive via fence 20 that circumscribe the antennaelements 14-2 and 14-3 electrically isolate the antenna elements 14-2and 14-3, respectively.

The test fixture assembly 12 also includes sensors 32 positioned withinthe cavities 26. Because they are within the cavities 26, the sensors32, like the antenna elements 14, are electrically isolated from oneanother, thereby enabling per antenna element 14 or per transmit orreceive chain measurements. In some embodiments, the sensors 32 detectsignals transmitted from the respective antenna elements 14. Thus, thesensor 32-1 detects the signal transmitted from the antenna element14-1, the sensor 32-2 detects the signal transmitted from the antennaelement 14-2, and the sensor 32-3 detects the signal transmitted fromthe antenna element 14-3. The signals detected by the sensors 32 areoutput to a controller 34. Notably, the signals may be pre-processed(e.g., downconverted and Analog-to-Digital (A/D) converted) in thesensors or by circuitry connected between the sensors 32 and thecontroller 34 prior to processing by the controller 34. The controller34 processes the signals to perform one or more measurements for each ofthe antenna elements 14 individually. The measurements may include, forexample, one or more of: an amplitude error, a phase error, outputpower, Error Vector Magnitude (EVM), and Adjacent Channel Leakage Ratio(ACLR). However, these measurements are only examples. Additional oralternative measurements may be performed.

In addition or alternatively, in some embodiments, receive measurements(e.g., noise figure measurements) are performed. For example, in someembodiments, the sensors 32 transmit, or inject, signals generated by,e.g., the controller 34. The injected signals are received by therespective antenna elements 14 and processed by the respective receivechains included within the SIAA 16 or external to the SIAA. Theprocessed signals are provided to the controller 34 and processed toperform one or more receive measurements for each of the antennaelements 14 individually. As another example, signals output by theantenna elements 14 may be processed to perform measurements when, e.g.,no signals are being injected by the sensors 32 at the antenna elements14.

The controller 34 may be implemented as hardware or a combination ofhardware and software. For example, the controller 34 may be implementedas one or more processors (e.g., Application Specific IntegratedCircuit(s) (ASIC(s)), Field Programmable Gate Array(s) (FPGA(s)),Digital Signal Processor(s) (DSP(s)), Central Processing Unit(s)(CPU(s)), and/or the like) and memory storing software instructions thatwhen executed by the processor(s) cause the controller 34 to operate asdescribed herein.

The test figure assembly 12 and the SIAA 16 also include mechanicalalignment features to provide proper and precise alignment between thesidewalls 30 of the cavities 26 and the electrically conductive viafence 20. In this example, the mechanical features include a groove 36in the surface of the substrate 18 around the periphery of the SIAA 16and a respective ridge 38 around the periphery of the test fixtureassembly 12. However, other mechanical alignment mechanisms (e.g., pinsand holes) may be used.

FIG. 2 illustrates a variation of the system 10 in which a dielectric40, or dielectric structure, is included on the surface of the SIAA 16and extends over the antenna elements 14 according to some embodimentsof the present disclosure. In some embodiments, the dielectric 40 is anon-removable or removable dielectric raydome. If the dielectric 40 isnon-removable, the dielectric 40 may, in some embodiments, cover the viafence 20, in which case the dielectric 40 may be doped in areas over thevia fence 20 to become electrically conductive in those areas. Thedielectric 40 includes one or more layers of a dielectric material. Thedielectric 40 protects the SIAA 16 and, in particular, the antennaelements 14. Normally, a thickness of the dielectric 40 would berelatively large. Such a thick dielectric would prevent the test fixtureassembly 12 from functioning as described herein. As such, in thisembodiment, the dielectric 40 is sufficiently thin and/or doped toenable sufficiently good capacitive coupling between the sidewalls 30 ofthe cavities 26 and the electrically conductive via fence 20 at adesired frequency of operation. In other words, the dielectric 40 issufficiently thin and/or doped, at least at the locations where thesidewalls 30 of the cavities 26 align with the electrically conductivevia fence 20, to be electrically conductive. In some embodiments, thethickness of the dielectric 40 is less than λ/4, where λ is a wavelengthof a carrier frequency to be transmitted or received by the SIAA 16. Insome alternative embodiments, the dielectric 40 is removable such thatthe dielectric 40 can be removed before attaching the test fixtureassembly 12 to the surface of the SIAA 16 for testing of the antennaelements 14. Once testing is complete, the test fixture assembly 12 canbe removed from the SIAA 16 and the dielectric 40 can be placed backonto the SIAA 16 for, e.g., normal operation. Alternatively, thedielectric 40 may or may not be removable and is not integrated onto theSIAA 16 until after testing using the test fixture assembly 12 iscomplete.

FIGS. 3A and FIGS. 3B and 3C illustrate a cross-sectional view andtop-down views of the SIAA 16 of FIG. 1, respectively, according to someexample embodiments of the present disclosure. This discussion isequally applicable to the embodiment of FIG. 2 other than showing thedielectric 40. As illustrated in FIG. 3A and as described above, theSIAA 16 includes the substrate 18, the antenna elements 14 on thesurface of the substrate 18, and the electrically conductive via fence20. In this example, the SIAA 16 further includes the ground plate 22within the substrate 18 to which the electrically conductive via fence20 is coupled. In addition, in this example, the SIAA 16 includes thegroove 36, which provides a mechanical alignment mechanism by which thesidewalls 30 of the cavities 26 of the test fixture assembly 12 (notshown) are properly aligned with the electrically conductive via fence20.

As illustrated in FIG. 3B, in this example, the electrically conductivevia fence 20 is formed by a number of vias 42 that extend from thesurface of the substrate 18 to the ground plate 22. In other words, oneend of each of the vias 42 is preferably exposed at the surface of thesubstrate 18 and the other end of each of the vias 42 is preferablycoupled to (electrically and, potentially, physically) the ground plate22. Each via 42 is a hole in the substrate 18 that is filled with asuitable material, which in this example is an electrically conductivematerial such as, e.g., metal. Note while the vias 42 have a squareshaped cross-section in this example, the vias 42 may have across-section of any desired shape such as, e.g., square, rectangular,circular, or the like. Further, the size of the vias 42, the number ofvias 42, and the spacing between the vias 42 may vary depending on theparticular implementation. Still further, while not illustrated, acontact pad(s) may be provided on the surface of the substrate 18 overthe vias 42 to enable or improve electrical and physical contact betweenthe sidewalls 30 of the cavities 26 of the test fixture assembly 12 andthe electrically conductive via fence 20. As can be seen in FIG. 3B, afirst portion of the electrically conductive via fence 20 circumscribesthe antenna element 14-1, a second portion circumscribes the antennaelement 14-2, and a third portion circumscribes the antenna element14-3.

It should be noted that the example of the electrically conductive viafence 20 illustrated in FIG. 3B is only an example. As another example,the electrically conductive via fence 20 may be formed by trenches intothe surface of the substrate 18, where the trenches are filled within asuitable material such as, e.g., an electrically conductive materialsuch as metal, as shown in FIG. 3C. Also, it should be noted that theshape of the antenna elements 14 shown in FIG. 3B is only an example.The shape of the antenna elements 14 may vary depending on theparticular implementation.

As can be also seen in FIGS. 3B and 3C, in this example, the groove 36extends around the periphery of the substrate 18. Again, the groove 36is only one example of a mechanical alignment mechanism. Othermechanical alignment mechanisms may be used as will be appreciated byone of ordinary skill in the art upon reading this disclosure.

FIGS. 4A and 4B illustrate a cross-sectional view and a bottom-up viewof the test fixture assembly 12 of FIG. 1, respectively, according tosome embodiments of the present disclosure. As illustrated in FIG. 4Aand as described above, the test fixture assembly 12 includes thefixture 24 and the one or more materials 28 within the fixture 24 thatform the cavities 26. In addition, the test fixture assembly 12 includesthe sensors 32 in the respective cavities 26. In this example, the testfixture assembly 12 also includes the ridge 38 that operates togetherwith the groove 36 in the surface of the SIAA 16 to provide propermechanical alignment between the sidewalls 30 of the cavities 26 and theelectrically conductive via fence 20.

As illustrated in FIG. 4B, in this example, the material(s) 28 areutilized to form the cavities 26. In particular, the cavity 26-1 hassidewalls 30-1, 30-2, 30-3, and 30-4 as well as an upper surface 44-1formed of the material(s) 28. The sensor 32-1 is, in this example,positioned on or near the upper surface 44-1 of the cavity 26-1. Thecavity 26-2 has sidewalls 30-3, 30-5, 30-6, and 30-7 as well as an uppersurface 44-2 formed of the material(s) 28. Note that, in this example,the cavities 26-1 and 26-2 share the common sidewall 30-3. The sensor32-2 is, in this example, positioned on or near the upper surface 44-2of the cavity 26-2. The cavity 26-3 has sidewalls 30-6, 30-8, 30-9, and30-10 as well as an upper surface 44-3 formed of the material(s) 28.Note that, in this example, the cavities 26-2 and 26-3 share the commonsidewall 30-6. The sensor 32-3 is, in this example, positioned on ornear the upper surface 44-3 of the cavity 26-3.

Although the concepts disclosed herein are more suitable for designs formillimeter wave applications, the concepts disclosed herein are notfrequency dependent upon millimeter wave. Any design which enables aconnection of a test fixture assembly 12 such as one including anelectrically conductive via fence 20 or wall between antenna elements 14or sub-arrays on the antenna board may use the concepts disclosedherein.

Note that the coupling transfer function for each cavity 26 is derivableand can be characterized and, as such, can be removed from therespective measurement. Further, each senor 32 provides an isolatedmeasurement of conducted signals. This enables isolated transmitperformance measurements for the active drive circuits of each antennaelement 14 (e.g., linearity, etc.), enables isolated receive performancemeasurements for the noise figure, and enables time cost saving byenabling simultaneous measurements for all of the antenna elements 14.Still further, the test fixture assembly 12 enables the measurementswithout the need for connectors, which reduces cost and complexity.Further, the additional cost for manufacturing the SIAA 16 is minimalsince only the addition of the electrically conductive via fence 20 and,optionally, the mechanical alignment mechanism is needed.

In the example embodiments above, the antenna elements 14 areillustrated as antenna elements 14 that are formed on the surface of thesubstrate 18. However, in some alternative embodiments, the antennaelements 14 are slots forming a slotted antenna. In this regard, FIG. 5illustrates one example of the SIAA 16 in which the antenna array is aslotted antenna array in which the antenna elements 14 are slots formedin a ground plane 46 on the surface of the substrate 18. Note that whilethe slots are shown as having a rectangular shape in the example of FIG.5, the shape of the slots will vary depending on the particularimplementation (i.e., the slots can have any shape). The ground plane 46is, at least in some embodiments, a metal layer that is connected toground within the substrate 18. The slots are referred to as slottedantenna elements 14. As will be appreciated by one of skill in the art,a microstrip or similar structure within the substrate 18 operates todrive or excite the slotted antenna elements 14 and/or receive signalsfrom the slotted antenna elements 14. While not illustrated in FIG. 5,the SIAA 16 also includes a mechanical alignment feature for aligningthe test fixture assembly 12 with the SIAA 16, as described above. Also,in this embodiment, the electrically conductive via fence 20 isoptional. As such, it is not shown. However, in some embodiments, theSIAA 16 using the slotted antenna array also includes the electricallyconductive via fence 20, as described above.

FIG. 6 is a cross-sectional view of the SIAA 16 of FIG. 5 and the testfixture assembly 12 according to some embodiments of the presentdisclosure. In this example, the SIAA 16 includes the electricallyconductive via fence 20 where the sidewalls 30 of the cavities 26 arealigned with the electrically conductive via fence 20, as describedabove. Again, note that the electrically conductive via fence 20 isoptional in this embodiment. More specifically, since the ground plane46 is already grounded, the test fixture 24 is grounded when thesidewalls 30 come into contact with the ground plane 46. As such, insome embodiments, the SIAA 16 does not include the via fence 20 sincethe sidewalls 30 of the test fixture 24 are already grounded.

As discussed above, the test fixture assembly 12 together with theelectrically conductive via fence 20 of the SIAA 16 enable per antennaelement measurements. With the knowledge of these per antenna elementmeasurements, one of many corrective steps can be taken. For example,during manufacture, the SIAA 16 may be rejected if the per antennaelement measurements indicate that any of the antenna elements 14 or anyof the respective transmit or receive chains fail some predefinedrequirement at the cost of the SIAA 16 and the time spent. However, asanother example, with the knowledge provided by the per antenna elementmeasurements obtained using the test fixture assembly 12, the SIAA 16could be shipped with information indicating the antenna element(s) 14and related circuitry that should not be used when the SIAA 16 isdeployed. This can be appropriate because, in antenna systems with alarge number of antenna elements 14, each antenna element's contributionto the overall performance of the antenna array is diminished. Otherexamples of corrective actions could be to include a map of relativegains or phase errors. This error information can be used by a system tocompensate for the manufactured quality of the SIAA 16.

In this regard, FIGS. 7 and 8 are flow charts that illustrate processesthat utilize measurements obtained using the test fixture assembly 12according to some embodiments of the present disclosure. In the processof FIG. 7, measurements are performed using the test fixture assembly 12(step 100). The measurements are per antenna element measurements suchas, for example, amplitude and/or phase error measurements for eachantenna element 14. However, any desired type of per antenna elementmeasurement may be performed. For example, for the transmit scenario, asignal(s) is(are) transmitted via the antenna elements 14. Duringtransmission, the sensors 32 sense the respective signals output by theantenna elements 14 and provide respective signals to, e.g., thecontroller 34. The controller 34 then processes the sensed signals toprovide the desired measurement(s). For example, amplitude and/or phaseerror measurements may be obtained by comparing (e.g., at baseband) thesensed signals to the respective signal(s) input to the transmit chainsdriving the antenna elements 14. As another example, for the receivescenario, the controller 34 may generate test signals and inject thetext signals into the cavities 26 through the sensors 32 and obtainresulting output signals of the receive chains of the respective antennaelements 14. Based on the resulting output signals, the controller 34may compute, e.g., noise figure measurements and/or receive sensitivitybased on the output signals. Note that the examples above arenon-limiting. Other types of measurements may be obtained in a similarmanner, as will be appreciated by one of ordinary skill in the art uponreading this disclosure.

The measurements are then utilized (step 102). For example, a controller(e.g., the controller 34) may perform the measurements in step 100 orobtain the measurements from a measurement system that performed themeasurements in step 100. The controller may then utilize themeasurements for, e.g., compensation of the antenna array implemented onthe SIAA 16 by, e.g., calibration of active components in the radio ortransceiver chain. For example, the controller may calibrate anamplitude and/or phase error for each antenna element 14 or respectivetransmit or receive chain using respective measurements. As anotherexample, the measurements may be utilized by providing the measurementsor information derived from the measurements to another entity (e.g., acustomer that will utilize the SIAA 16 in a system). This informationmay include, for example, the measurements or information that indicateswhich antenna elements 14 or which transmit or receive chain does notmeet some predefined performance requirement. This information may beprovided, e.g., by the manufacturer to, e.g., a customer or purchaser ofthe SIAA 16.

FIG. 8 is a flow chart that illustrates a process for obtaining andusing information related to measurements performed on the antennaelements 14 of the SIAA 16 according to some embodiments of the presentdisclosure. This process may be performed by, e.g., a customer and/or asystem implemented by a customer that purchases or otherwise acquiresthe SIAA 16 from the manufacturer. As illustrated, the SIAA 16 andinformation related to measurements performed on the antenna elements 14are obtained (step 200). The measurements are per antenna elementmeasurements performed using, e.g., the test fixture assembly 12, asdescribed above. The information may be the measurements or informationderived from the measurements, as described above. The information isthen utilized (step 202). For example, the information may be utilizedby, e.g., a controller in a system in which the SIAA 16 is integratedto, e.g., avoid the use of any antenna elements 14 that do not meet apredefined performance requirement and/or perform a compensation orcalibration process by which non-ideal characteristics of the SIAA 16,as indicated by the information, are mitigated. For instance, theinformation may indicate an amplitude and/or phase error for eachantenna element 14 and the system may operate to compensate foramplitude and/or phase error of at least some of the antenna elements14.

The following acronyms are used throughout this disclosure.

3GPP Third Generation Partnership Project

5G Fifth Generation

SIAA Substrate Integrated Antenna Array

ACLR Adjacent Channel Leakage Ratio

A/D Analog-to-Digital

ASIC Application Specific Integrated Circuit

CPU Central Processing Unit

dB Decibel

DSP Digital Signal Processor

EIRP Equivalent Isotropically Radiated Power

EIS Effective Isotropic Sensitivity

EVM Error Vector Magnitude

FPGA Field Programmable Gate Array

GHz Gigahertz

PCB Printed Circuit Board

RF Radio Frequency

Those skilled in the art will recognize improvements and modificationsto the embodiments of the present disclosure. All such improvements andmodifications are considered within the scope of the concepts disclosedherein.

1-11. (canceled)
 12. A system comprising: a Substrate Integrated AntennaArray Substrate, SIAA, comprising: a substrate; and one or more antennaelements at a surface of the substrate; and a test fixture assemblycomprising one or more cavities formed of one or more materialsproviding electrical isolation, wherein the test fixture assembly ispositioned on the surface of the substrate of the SIAA such that, foreach cavity of the one or more cavities, sidewalls of the cavitycircumscribe a respective one of the one or more antenna elements suchthat the one or more cavities electrically isolate the one or moreantenna elements.
 13. The system of claim 12 wherein the one or moreantenna elements comprise a plurality of antenna elements, and the oneor more cavities comprise a plurality of cavities.
 14. The system ofclaim 12 wherein the one or more antenna elements are antenna elementson the surface of the substrate.
 15. The system of claim 12 wherein theone or more antenna elements are slotted antenna elements formed in aground plane on the surface of the substrate.
 16. The system of claim 12wherein: the SIAA further comprises an electrically conductive via fencehaving a first side electrically coupled to ground within the substrateand a second side at the surface of the substrate, the electricallyconductive via fence separately circumscribing each antenna element ofthe one or more antenna elements within the substrate; and the testfixture assembly is positioned on the surface of the substrate of theSIAA such that, for each cavity of the one or more cavities, thesidewalls of the cavity are aligned with and electrically coupled tosections of the electrically conductive via fence that circumscribe arespective one of the plurality of antenna elements such that the viafence and the one or more cavities electrically isolate the one or moreantenna elements.
 17. The system of claim 12 wherein the sidewalls ofthe cavity are in physical contact with the sections of the electricallyconductive via fence that circumscribe the respective one of the one ormore antenna elements.
 18. The system of claim 16 wherein: theelectrically conductive via fence comprises a plurality of electricallyconductive vias each having a first end coupled to ground within thesubstrate and a second end at the surface of the substrate, theplurality of electrically conductive vias positioned in the substratesuch that each antenna element of the one or more antenna elements isseparately circumscribed by a respective subset of the plurality ofelectrically conductive vias; and the test fixture assembly ispositioned on the surface of the substrate of the SIAA such that, foreach cavity of the one or more cavities, the sidewalls of the cavity arealigned with and electrically coupled to the subset of the plurality ofelectrically conductive vias that circumscribe a respective one of theone or more antenna elements such that the electrically conductive viafence and the one or more cavities electrically isolate the one or moreantenna elements.
 19. The system of claim 18 wherein the sidewalls ofthe cavity are in physical contact with the subset of the plurality ofelectrically conductive vias that circumscribe the respective one of theone or more antenna elements.
 20. The system of claim 12 wherein theSIAA further comprises a dielectric on a surface of the one or moreantenna elements opposite the substrate.
 21. The system of claim 20wherein a thickness of the dielectric is less than λ/4, where λ is awavelength of a carrier frequency to be transmitted or received by theSIAA.
 22. The system of claim 12 further comprising a mechanicalalignment mechanism that aligns the test fixture assembly with the SIAAsuch that the one or more cavities in the test fixture assembly arealigned with the one or more antenna elements, respectively.
 23. Thesystem of claim 22 wherein the mechanical alignment mechanism comprises:a groove around a periphery of one of the SIAA and the test fixtureassembly; and a ridge around a periphery of the other one of the SIAAand the test fixture assembly.
 24. The system of claim 12 wherein thetest fixture assembly further comprises one or more sensors in the oneor more cavities, respectively.
 25. The system of claim 24 furthercomprising a controller that processes signals output by the one or moresensors during transmission of signals from the one or more antennaelements to perform one or more measurements for each of the one or moreantenna elements.
 26. The system of claim 25 wherein the one or moremeasurements comprise at least one of a group consisting of: amplitudeerror, phase error, output power, error vector magnitude, and adjacentchannel leakage ratio.
 27. The system of claim 24 further comprising acontroller that generates signals that are injected into the one or morecavities by the one or more sensors and processes one or more resultingsignals output by the one or more antenna elements or one or morerespective receive chains to perform one or more receive measurementsfor each of the one or more antenna elements.
 28. The system of claim 27wherein the one or more receive measurements comprise at least one of agroup consisting of: noise figure and receive sensitivity.